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U.S. Department of Energy
Office of Scientific and Technical Information

Ultra-low NO sub x gas turbine combustor. Final report, October 1985-June 1990

Technical Report ·
OSTI ID:5595805
The design and rig testing of a lean premixed, low emissions, gas turbine combustor prototype are described. The combustor evaluated was a 90 degree sector of a full-scale annular combustor for a 3.7 Mw, natural gas-fired, industrial gas turbine. The combustor sector represented an intermediate development step in extending the lean premixed combustor technology from a can combustor configuration with a single fuel injector to an annular geometry with multiple injectors. In a parallel effort, a rich/lean combustor sector was also evaluated. This effort provided a direct comparison of the NO{sub x} reduction capabilities of the rich/lean and lean premixed concepts. Testing at typical gas turbine operating pressures (122 psig) demonstrated that both the lean premixed and rich/lean combustor sectors were capable of meeting the program NO{sub x} goal of 25 ppm (15% O{sub 2}) while maintaining CO emissions below 50 ppm. The testing indicated that variable geometry and fuel staging will be required for low emissions range extension and low part load operation, respectively.
Research Organization:
Solar Turbines, Inc., San Diego, CA (United States)
OSTI ID:
5595805
Report Number(s):
PB-91-184994/XAB; SR--90-R-5357-45; CNN: GRI-5083-251-1000
Country of Publication:
United States
Language:
English